The purpose of the present invention is to provide a fuel tank, main wings, an aircraft fuselage, an aircraft, and a moving body, which enable working hours and costs involved in a manufacturing process to be reduced, and weight increases to be prevented. The fuel tank comprises a structural member in which carbon fiber reinforced plastic (CFRP) (15) is used, the carbon fiber reinforced plastic (CFRP) (15) comprising a reinforcing material that includes carbon fibers and a matrix that includes plastic. The structural member is formed by laminating a conductive sheet (17) between prepregs of the carbon fiber reinforced plastic (CFRP) (15). In this case, a cut surface (11a) of the structural member formed by cutting the structural member may be exposed on the inside in which fuel is stored.


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    Title :

    ТОПЛИВНЫЙ БАК, ОСНОВНЫЕ КРЫЛЬЯ, КОРПУС ЛЕТАТЕЛЬНОГО АППАРАТА, ЛЕТАТЕЛЬНЫЙ АППАРАТ И ТРАНСПОРТНОЕ СРЕДСТВО


    Publication date :

    2017-05-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B60K Anordnung oder Einbau von Antriebseinheiten oder von Kraft- bzw. Drehmomentübertragungen in Fahrzeugen , ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT